What Is High Cycle Fatigue

What is considered high cycle fatigue?

When the fatigue occurs above 103 cycles (usually 104 or more), it is usually called High-cycle fatigue The material is subject to lower loads, usually less than 2/3 of the yield stress The deformation is in elastic range The fatigue life is “high-cycle” (103 ~ 106)

What is high cycle fatigue and low cycle fatigue?

High cycle fatigue require more than 104 cycles to failure where stress is low and primarily elastic Low cycle fatigue is characterized by repeated plastic deformation (ie in each cycle) and therefore, the number of cycles to failure is low

What is meant by low cycle fatigue?

LCF is a type of fatigue caused by large plastic strains under a low number of load cycles before failure occurs High stresses greater than the material yield strength are developed in LCF due to mechanical or thermal loading The stresses may exceed the yield strength and cause large plastic deformation

What are the three stages of fatigue?

There are three stages of fatigue fracture: initiation, propagation, and final rupture Indeed, this is the way that most authors refer to fatigue fracture, for it helps to simplify a subject that can become exceedingly complex

What causes high cycle fatigue?

Durability and reliability in diesel engine system design High cycle fatigue is a type of fatigue caused by small elastic strains under a high number of load cycles before failure occurs The stress comes from a combination of mean and alternating stresses

When fatigue occurs above _ cycles it is called high cycle fatigue?

Explanation: When fatigue takes place above 103 cycles, it is referred as a high cycle fatigue

What decreases the fatigue strength?

Decarburisation diminishes the fatigue resistance of steel components by: diminishing the local fatigue strength due to the decreased density of the surface layer, increased grain size and diminished fracture toughness and yield strength (Chernykh 1991; Todinov, 2000b)

How do I know if I have fatigue failure?

A quick analysis of the fracture surface of a fatigue failure will often show features casually referred to as “beach marks” These indicate the propagation of the failure from the initial cracks Once the crack size has reached a critical level, it will propagate very rapidly until the fracture is complete

How can I improve my fatigue life?

Fatigue life is improved by reducing the stress concentration on the weld joint, softening the weld toe shape, improving the metal structure of the weld zone, and adequately changing the pin shape and treatment conditions of friction stir welding as shown in Figure 2

What causes material fatigue?

Fatigue is the result of residual stress affecting an asset’s composition, including stresses from temperature, corrosion, load, and a variety of other factors Over time, assets of every material experience fatigue-related wear from operational use and the conditions of their surrounding environment

What are the characteristics of low cycle fatigue?

Low cycle fatigue has two fundamental characteristics: plastic deformation in each cycle; and low cycle phenomenon, in which the materials have finite endurance for this type of load

What is Coffin Manson Law?

The Coffin–Manson law relates for a metal uniaxially and cyclically loaded the plastic strain amplitude ɛp to the cycle number of fracture Nf through a two-parameter power law(1) ε p = ε f N f c where ɛf and c (<0) are the fatigue ductility coefficient and exponent, respectively [1], [2]

How do you test for fatigue?

To perform a fatigue test a sample is loaded into a fatigue tester or fatigue test machine and loaded using the pre-determined test stress, then unloaded to either zero load or an opposite load This cycle of loading and unloading is then repeated until the end of the test is reached

What is fatigue cracking?

Fatigue cracking is one of the primary damage mechanisms of structural components Fatigue cracking results from cyclic stresses that are below the ultimate tensile stress, or even the yield stress of the material This leaves tiny steps in the surface that serve as stress risers where tiny cracks can initiate

Where does fatigue crack start?

Fatigue cracks in typical aircraft alloys usually start from statistically distributed small material discontinuities or surface defects Over a low stress concentration region, the largest crack that dictates fatigue life is often the fastest growing crack that starts from one of the worst discontinuities

How do cracks form in high cycle fatigue?

How fatigue cracks grow Initiation of cracks due to local plasticity, often caused by stress concentrations, local surface roughness, wear damage at contacts etc Lower yield stress materials more prone to fatigue at a given stress level

What is notch sensitivity?

The notch sensitivity of a material is a measure of how sensitive a material is to notches or geometric discontinuities Notch sensitivity is influenced by many parameters such as notch geometry The results show that the notch geometry has profound effect on fatigue life of materials

In what terms fatigue life is measured?

Explanation: Fatigue life is measured in terms of the number of cycles of failure The maximum stress is kept fixed

What is reversed stress?

A purely reversing or cyclic stress means when the stress alternates between equal positive and negative peak stresses sinusoidally during each cycle of operation, as shown This kind of cyclic stress is developed in many rotating machine parts that are carrying a constant bending load

What does metal fatigue look like?

Stage One: After a certain amount of load cycles, micro-cracks begin to form on the metal during the metal fatigue process The micro-cracks tend to form around stress concentrating geometric features such as edges The crack surface will be different in appearance depending on metal type and metal tensile strength

What type of stresses cause fatigue failure?

Fatigue failure occurs due to cyclic stress from operating conditions The main mechanisms of failure occur from mechanical fatigue or thermal fatigue The tipping point for failure is when the material fails at loads lower than the yield strength of the material